JASC 5510
Service difficulty reports · 5,966
Reports filed under 5510 · Horizontal Stabilizer Structure, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5510' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5510' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR P2EA000234Panel · dentedMIC - DURING A WALK AROUND INSPECTION, FOUND BIRD STRIKE ON RIGHT HORIZONTAL STAB, DEFECT SIZE 19 INCHES LONG BY 5.5 INCHES WIDE, 1.75 INCHES DEEP. REPLACED LEADING EDGE PANEL PER SRM 55-10-0. (M)SDR CALA0001216Fairing · chafedINSPECTION FOUND UPPER RT HORIZONTAL STABILIZER FAIRING CRACKED AT FORWARD UPPER END AND CHAFING IN THREE AREAS AT FORWARD UPPER END AND DELAMINATION NEAR CENTER OF UPPER EDGE OF FAIRING. THE ANGLE WAS REMOVED AND A REPAIR ANGLE, DOUBLER, AND FILLER WERE INSTSDR CALA0001212Structure · gougedINSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD UPPER AND LOWER BARREL NUT HOLES GOUGED. REAMED BARREL NUT HOLES AND INSTALLED BUSHINGS IAW EA 9-5511-2-A0738 AND ECRA 5511-01029.SDR MWEA00641Fitting · crackedMKE - HORIZONTAL STABILIZER CENTER SPAR BOX UPPER AFT GRILL PLATE FITTING HAS A CRACK EMINATING FROM THE FAR LEFT FASTENER HOLE ON THE HORIZONTAL PLANE. FABRICATED AND INSTALLED FITTING. (M)SDR CALA0001200Angle · crackedINSPECTION FOUND A CRACK IN RADIUS OF FORWARD MOUNTING FLANGE AT UPPER RT HORIZONTAL STABILIZER FAIRING. REMOVED ANGLE FROM FAIRING AND INSTALLED A NEW ANGLE IAW SRM 51-30-2, 51-10-2, 55-12-0, FIGURE 7A, 51-10-3, 51-30-0, AND 51-20-0.SDR 20000821SH011Bolt · rustedDURING ANNUAL INSPECTION, FOUND THE HORIZONTAL STABILIZERS TO CREAK WHEN FORCED UP OR DOWN. DURING INVESTIGATION, NOTICED MOVEMENT IN THE AFT ATTACH FITTING FOR BOTH SIDES. REMOVED THE BOLTS FROM THEIR CLOSE TOLERANCE HOLES TO DISCOVER THEY WERE TOO SHORT. SDR UPS00433726Fitting · corrodedINSPECTION TYPE:C, RT HORIZONTAL STABILIZER INTERIOR CORROSION FOUND ON A RIGHT ANGLE FITTING AT STAB STA 243, BETWEEN REAR SPAR AND S1 UPPER SURFACE. PLEASE INVESTIGATE NEW FITTING, FABRICATED IAW E0100940 AND FITTED IAW SRM 51-30-02.SDR QXEA0002225Fastener · loosePDX- RIGHT VERTICAL CONNECTION ANGLE HAS LOOSE AND SMOKING HI-LOKS AND BUTTON HEAD RIVETS AT AFT SPAR. REPAIRED IAW FOKKER SRM 51-30-02 AND HORIZON AIR EA 4-55-247.SDR QXEA0002220Fastener · loosePDX- LEFT VERTICAL CONNECTION ANGLE HAS LOOSE HI-LOKS AND BUTTON HEAD RIVETS AT AFT SPAR. REPAIRED IAW FOKKER SRM 51-30-02, SRM 51-31-01 AND HORIZON AIR EA 4-55-247.SDR USAA001122Bushing · corrodedCLT - FOUND LUG AND BUSHING CORRODED .25 INCH, LEFT HORIZONTAL STAB LOWER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1 C-53-701-02. REMOVED CORROSION PER SRM 55-10-10. (M)SDR USAA001121Bushing · corrodedCLT - FOUND LUG AND BUSHING CORRODED .25 INCH, LEFT HORIZ STAB UPPER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1. REMOVED CORROSION PER SRM 55-10-10. (M)SDR USAA001126Stiffener · crackedFOUND VERTICAL STIFFENER WITH A .375 INCH CRACK, STAB STATION 101.90 BETWEEN RIVETS. REPLACED STIFFENER AND INSTALLED PER SRM 51-10-02 AND 55-10-01. (M)SDR USAA001086Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED 1 INCH, HORIZ STAB CENTER BOX LOWER CHORD TO WEB. INSTALLED NEW ANGE PER TR 51-10-02. (M)SDR DHL200072143CStructure · damagedLEFT HORIZ STAB TIP UPPER SURFACE DAMAGED. REMOVED LT HORIZ STAB TIP AND ROUTED TO F/G SHOP PER SRM 51-30-2. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8. REINSTALLED TIP ON STAB PER SRM 51-30-2.SDR CALA0001194Fairing · crackedINSPECTION FOUND A 1 INCH CRACK IN LEFT I/B LEADING EDGE HORIZONTAL STABILIZER FAIRING. THE OLD DOUBLER WAS REMOVED, THE CRACK WAS STOP DRILLED, AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-30-02.SDR 00FDEA00501Fastener · brokenRT HORIZ STAB PIVOT SUPPORT, LOWER HALF, HAS 2 BROKEN FASTENERS WHERE PRIMARY AND SECONDARY ATTACH TO UPPER EDGE OF LOWER TORQUE BOX. (Y) 2122.8 (X) -41.7 INSIDE DOOR 316BB. *S/D* REMOVED AND REPLACED FASTENERS PER SRM 53-00-01.SDR UPS00833496Fitting · crackedINSPECTION TYPE:C123, LEFT HORIZONTAL STAB L/E LOWER ATTACH FLANGE FITTING IS CRACKED AT XFS 60. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21.SDR QXEA0002147Fitting · corrodedPDX- FRETTING CORROSION DAMAGE ON HORIZONTAL STABILIZER JUNCTION FITTING OF LEFT HAND UPPER LUG. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-4 PAGE 9 AND HORIZON AIR EA 4-55-245.SDR QXEA0002146Fitting · corrodedPDX- FRETTING CORROSION DAMAGE ON HORIZONTAL STABILIZER JUNCTION FITTING OF LEFT HAND LOWER LUG. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-4 PAGE 9 AND HORIZON AIR EA 4-55-245.SDR QXEA0002145Fitting · corrodedPDX- FRETTING CORROSION DAMAGE ON HORIZONTAL STABILIZER JUNCTION FITTING OF RIGHT HAND UPPER LUG. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-4 PAGE 9 AND HORIZON AIR EA 4-55-244.SDR QXEA0002144Fitting · corrodedPDX- FRETTING CORROSION DAMAGE ON HORIZONTAL STABILIZER JUNCTION FITTING OF RIGHT HAND LOWER LUG. REPAIRED IAW FOKKER SRM 55-01-01, 51-10-4 PAGE 9 AND HORIZON AIR EA 4-55-244.SDR COMA0060607Bushing · wornHORIZONTAL STAB BUSHINGS LEFT I/B, LT O/B, AND RIGHT I/B AND RIGHT O/B WERE FOUND TO HAVE WEAR DAMAGE, RIGHT O/B REQUIRED 3RD OVERSIZE. REMOVED AND REPLACED BUSHINGS IN HORIZONTAL STAB IAW CRJ REO 601R-555-11-041 AND REO 601R-55-11-022 REV A.SDR CALA0001121Fairing · crackedINSPECTION FOUND A 2 INCH CRACK IN RT HORIZONTAL STABILIZER BANANA FAIRING. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 55-01 AND 55-01-1.SDR ABXA000383Fitting · crackedHORIZONTAL STABILIZER BOX SECTION FITTING CRACKED AT PANEL NR 3902. REPLACED FITTING IAW DC9 SRM.SDR CA000802017Tip Cap · cracked(CAN) DURING FLIGHT A VIBRATION WAS FELT IN THE FLOOR AND WENT AWAY AS THE AIRCRAFT WAS RETURNING TO THE LANDING SITE. THE ENGINEER INSPECTED THE AIRCRAFT AND FOUND THE TIP PLATE OF THE R/H SIDE OF THE HORIZONTAL STABILIZER WAS MISSING.SDR CA000719023Bracket · cracked(CAN) WHILE INSPECTING VERTICAL STABILIZER LEADING EDGE IMPACT ON SKIN, A CRACK WAS IDENTIFIED ON THE LEFT HAND HORIZONTAL STABILIZER ATTACH BRACKET. NDT BY EDDY CURRENT METHOD CONFIRMED A .0625 INCH CRACK EMANATING FROM A WELD TERMINATION OF A DOUBLER ON BRSDR ASAA0040097Strap · chafedPAE - DURING SCHEDULED SI CHECK, THE RIGHT HORIZONTAL STABILIZER L/E WAS FOUND TO BE CHAFED ON THE INTERNAL STRAP AT INBOARD END, L/E STATION 86.88. REPAIRED PER EA 5510-01098. (M)SDR QXEA0001977Fitting · corrodedPDX- LEFT HAND UPPER AND LOWER LUGS OF HORIZONTAL STABILIZER JUNCTION FITTING HAVE PITTING CORROSION ON INBOARD AND OUTBOARD FACES. REPAIRED IAW HORIZON AIR EA 4-55-230.SDR QXEA00001976Fitting · corrodedPDX- RIGHT HAND UPPER AND LOWER LUGS OF HORIZONTAL STABILIZER JUNCTION FITTING HAVE PITTING CORROSION. REPAIRED IAW HORIZON AIR EA 4-55-231.SDR SWAA001182Fitting · corrodedDURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB REAR SPAR LUG BORE ATTACH FITTING CORRODED. REPAIRED FITTING PER ER NR 00-0643SDR SWAA001166Fitting · corrodedDURING SCHEDULED D CHECK, FOUND LT HORIZONTAL STAB HINGE HOUSING LOWER INBD AND OUTBD LUGS CORRODED. REPAIRED LUGS PER ER 00-0590.SDR CA000801014Bracket · cracked(CAN) THE BRACKET ON THE LEFT STABILIZER WAS CHANGED AS IT WAS FOUND TO BE CRACKED. P/N 0712302-1 WAS REPLACED WITH NEW PART USING EXISTING RIVET SIZE AND PATTERN.SDR 20000626SH013Bracket · crackedDURING 100-HOUR ANNUAL INSPECTION, THE HORIZONTAL STABILIZER ATTACHMENT POINT REINFORCEMENT ON LEFT SIDE WAS FOUND CRACKED. SUSPECTED CAUSE WAS PART HIGH TIME. ALTHOUGH THE RIGHT REINFORCEMENT WAS NOT CRACKED, IT WAS REPLACED DUE TO HIGH TIME. (X)SDR AWXA0000394Angle · crackedLEFT HORIZONTAL STABILIZER LOWER WEB ATTACH ANGLE CRACKED AT LOWER FORWARD LEADING EDGE SPAR, 4 FT FROM STABILIZER TIP. STOP DRILLED CRACK IAW SRM 55-10-09. CHECKED TERMINATION BY NDT. FABRICATED REPAIR ANGLES AND FILLERS IAW SRM 55-10-09, FIG 202. INSTALLSDR 20000613SH013Bracket · crackedTHREE OF FOUR BALANCE WEIGHT SUPPORT BRACKETS WERE CRACKED ALONG THE BEND RADIUS. CRACKS WERE 1.25 INCHES, 1.50 INCHES, AND 1.75 INCHES ON EACH. THIS WAS NOTICED DURING STABILIZER BEARING REPLACEMENT WITH THE STABLIZER OFF THE AIRCRAFT. SUBMITTER RECOMMENDESDR 20000613SH012Bracket · crackedTHREE OF FOUR BALANCE WEIGHT SUPPORT BRACKETS WERE CRACKED ALONG THE BEND RADIUS. CRACKS WERE 1.25 INCHES, 1.50 INCHES, AND 1.75 INCHES ON EACH. THIS WAS NOTICED DURING STABILIZER BEARING REPLACEMENT WITH THE STABLIZER OFF THE AIRCRAFT. SUBMITTER RECOMMENDESDR 20000613SH011Bracket · crackedTHREE OF FOUR BALANCE WEIGHT SUPPORT BRACKETS WERE CRACKED ALONG THE BEND RADIUS. CRACKS WERE 1.25 INCHES, 1.50 INCHES, AND 1.75 INCHES ON EACH. THIS WAS NOTICED DURING STABILIZER BEARING REPLACEMENT WITH THE STABLIZER OFF THE AIRCRAFT. SUBMITTER RECOMMENDESDR MALA000413Structure · dentedFOUND DURING C-CHECK, DENT AT LT HORIZONTAL STABILIZER LOWER SURFACE. MAINTENANCE INSPECTED AND FOUND 3 SEPARATE DENTS WITHIN 1 INCH OF EACH OTHER. REPAIRED PER REF: SAAB STATEMENT NR 72SDS2603.SDR 0002169623Angle · crackedHORIZONTAL STABILIZER LEADING EDGE I/B SECTION ANGLE AT LEADING EDGE FROM HOT AIR TUNNEL TO I/B WEB CRACKED. L/P 1448749. REPAIRED PER EA 96-172510.SDR UPS00832954Angle · crackedINSPECTION TYPE:C2, LT HORIZONTAL STAB ANGLE FWD OF FRONT SPAT AT HORIZONTAL ROOT CRACKED. REMOVED CRACKED ANGLE VERTICAL TRACK PER DC8 SRM 51-3-0, 51-1-21, 51-1-20D. FABBED AND INSTALLED NEW ANGLE PER DAC DWG 5654501 AND DC8 SRM 51- 1-21-, 51-1-20D. ALODINSDR 20000619SH028Attach Fitting · crackedDURING ANNUAL INSP, LT SIDE HORIZONTAL STABILIZER ATTACH BRACKET WAS FOUND CRACKED NEXT TO A MOUNT BOLT. APPROX ONE YEAR PRIOR, THE HORIZ STAB HAD BEEN REBUILT. THE SPAR, STRINGERS, AND SKIN HAD BEEN REPLACED. VERY FEW OF THE ORIGINAL PARTS WERE RETURNED TOSDR QXEA0001632Bracket · crackedYYC- STAB DRIVE FITTING HAS CRACKED BRACKET BETWEEN FORWARD LUGS ON BOTTOM SIDE. REPAIRED IAW FOKKER SRM 51-31-01.SDR CALA0000766Fairing · crackedINSPECTION FOUND A 2 INCH CRACK IN RT VERTICAL STABILIZER BANANA FAIRING. THE CRACKED AREA WAS REMOVED AND A FILLER AND DOUBLER WERE INSTALLED IAW SRM 55-01, FIGURE 2 AND 55-03, FIGURE 17.SDR CA000530041Bracket · cracked(CAN) UPON INSPECTION OF THE HORIZONTAL STABILIZER ATTACH BRACKET, IT WAS DISCOVERED THAT THE CASTING WAS CRACKED IN THE WEB BY THE ATTACH HOLES.SDR 20000613SH003Attach Fitting · corrodedINTERNAL CORROSION CAUSED FAILURE OF HORIZONTAL STABILIZER STRUT AT LOWER ATTACH FITTING. SUBMITTER RECOMMENDED LOWER ATTACH POINT DESIGNED SIMILAR TO UPPER FITTING AND LINSEED OIL APPLIED TO INSIDE OF STRUT. (X)SDR AT0000339Structure · chafedDURING A SCHEDULED INSPECTION, FOUND LEFT HORIZONTAL STABILIZER BETWEEN ELEVATOR STATION 195 AND 213 CHAFED OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR IAW 737 SRM 51-10-01.SDR CA000518016Bracket · cracked(CAN) DURING INSPECTION FOR AD 80-11-04, THE STEEL BRACKET THAT THE SUBJECT NUTPLATES ARE ATTACHED TO WAS FOUND TO BE CRACKED. THE CRACK COMPLETELY ENCIRCLED THE RIGHT UPPER NUTPLATE.SDR CA000511019Bracket · cracked(CAN) CRACK FOUND DURING INSPECTION IN WEBBING. SUBMITTER STATED THIS IS A COMMON AREA FOR CRACKING WITH THE UNITS.SDR 00FDEA00331Angle · crackedRIGHT HORIZONTAL STABILIZER CTR LEAD EDGE TEE ANGLE CRACKED. LEFT HORIZONTAL STAB CTR LEAD EDGE TEE ANGLE CRACKED. *S/D* REMOVED AND REPLACED PER 51-31-01 VOL II.SDR DL72K000936Hinge Fitting · corrodedTHE HORIZONTAL STABILIZER REAR SPAR HINGE FITTING LUGS WERE FOUND WORN ON THE LT AND RT I/B LUG FACES. THE LT I/B LUG FACE WAS SPOTFACED 0.010 AND THE RT I/B LUG FACE WAS SPOTFACED 0.015 TO REMOVE THE WEAR. THE LT I/B LUG BORE WAS REAMED TO 2.2345 DIA AND TH
Back to JASC 5510